1.0 SCIENCE INVESTIGATION AND INVESTIGATION PLAN
1.1 SUMMARY
The Imager for Magnetopause-to-Aurora Global Exploration
(IMAGE) will produce forefront science by quantifying the response of the magnetosphere to the time variable solar wind. It will acquire, for the first time, a variety of three-dimensional images of magnetospheric boundaries and plasma distributions extending from the magnetopause to the inner plasmasphere. The images will be produced on time scales needed to answer important questions about solar wind - magnetosphere interactions.
In its report, "Space Science in the Twenty-First Century: Imperatives for the
Decades 1995 to 2015," the Task Group on Solar and Space Physics of the Space
Science Board identified four key questions for magnetospheric physics:
During the study phase, a strawman payload and model spacecraft design
were identified to accomplish the IMI science objectives. Developing needs for
lower-cost spacecraft led to a final report on a descoped mission,
Magnetosphere Imager (MI), which still embodied the critical techniques of
neutral atom imaging (1 keV to 200 keV) and 30.4 nm imaging, along with
imaging of the global aurora and the geocorona. This mission would indeed yield
the first global views of the magnetosphere, specifically of the build-up and decay
of the ring current and the erosion and refilling of the plasmasphere, along
with the contextual measurements and link to ISTP that would be provided
by auroral imaging.
As defined, MI would fall short of answering two key questions identified in
the Space Science in the Twenty-First Century report to which it is potentially
very relevant: 1. How does the solar wind couple to the magnetosphere? and
2. What is the origin and fate of magnetospheric plasmas? Question 1 requires
quantitative measurements of the structure of the magnetopause, while
question 2 requires images of both the ionospheric source and the solar wind
source of magnetospheric plasma. MI would make no measurements of the
magnetopause, nor would its lower energy limit for magnetospheric ion imaging
(1 keV) be low enough to trace the ionospheric plasma back to its source. On
the other hand, our proposed IMAGE mission, while accomplishing the complete MI
objectives, will also utilize two techniques recently developed by the IMAGE team
to address effectively both of these questions.
The first technique is radio plasma imaging (RPI), which senses plasma
densities between 0.1 and 105 cm-3 and images plasma
boundaries globally throughout the magnetosphere on a one-minute time scale.
Thus, for example, the global topology of the magnetopause and the structure
of its interior boundary layer will be imaged continuously as they respond
to changes in the solar wind and interplanetary magnetic field, addressing
a crucial aspect of question 1 above.
The second new technique employed by IMAGE is the extension of neutral
atom imaging down to an energy of 10 eV by using a surface conversion
technique for converting low-energy neutral atoms into ions for energy
and mass analysis. This low energy coverage is essential for addressing
the origin of magnetospheric plasmas. The ionosphere is the source of a
large portion of magnetospheric plasmas, and the injection of ionospheric
ions into the magnetosphere can only be traced by imaging down to these energies.
With its unique instrument complement, the IMAGE mission will address
the high-priority magnetospheric physics objectives in ways not accessible
to the MI mission. It will obtain global images from the magnetopause to the
aurora, sensing changes in solar-wind conditions as reflected by magnetopause
topology and tracing both the solar-wind source and the ionospheric source of
magnetospheric plasmas. The IMAGE instrumentation has been chosen because it
has optimum performance in every parameter range, has been developed by
experienced scientific teams with extensive successful flight history,
is flight-proven to the maximum extent possible, and has been prototyped
and verified on the ground wherever new techniques are required.
The IMAGE spacecraft has been designed by GSFC using off-the-shelf
components from the FAST spacecraft, with a GSFC/Resource Analysis
Office (RAO) official cost estimate well below the MIDEX requirement.
The IMAGE mission represents a very low risk MIDEX with very high
scientific payoff. It complies with all MIDEX requirements for spacecraft
resources (mass, power, and data rate), mission schedule, mission costs and
contingencies. The IMAGE Science Team will claim no proprietary rights and
is committed to providing open access to all IMAGE data and an extensive
program of education and public outreach based directly upon programs
already implemented by IMAGE team members.
The report noted that the only practical post-ISTP approach to
testing of global magnetospheric models is one that utilizes techniques to
provide global images of the magnetosphere. In the subsequent Space Physics
Strategy Implementation Study [1991], the Inner Magnetosphere Imager (IMI)
mission was given highest priority for magnetospheric physics with the
realization that the techniques of neutral atom imaging and ultraviolet
imaging of He+ at 30.4 nm are well enough developed to provide global
images of regions such as the ring current and plasmasphere.
Imager | Measurement | Critical Measurement Requirements |
---|---|---|
NAI (LENA) |
Neutral atom composition and energy-resolved images from: 10-300 eV | FOV -90o x 90o. Angular Res. - 8o X 8o. Composition - distinguish H, He and O in ion outflow and interstellar neutrals. Energy Resolution - 0.8. Image Time - 5 min. Sensitivity - Effective area > 1cm2. |
NAI (MENA, HENA) |
Neutral atom composition and energy resolved images. MENA - 1-30 keV HENA - 10-200 keV |
FOV - 90o x 90o (image ring current from apogee.) Angular Res. - 8o X 8o. Composition - seperate solar wind (H) and magnetospheric (0) sources. Energy Resolution - 0.8 (MENA), 0.7 (HENA). Image Time - resolve substore processes (5 min.) Sensitivity - Effective area > 1cm2 (See Fig. 1.2.4). |
EUV | 30.4 nm imaging of plasmasphere He+ column densities | FOV - image plasmasphere from apogee (90o x 90o). Spatial Resolution - 0.1 Earth radii from apogee. Image Time - resolve plasmaspheric processes (several min - hours). |
FUV | Far ultraviolet imaging of the geocorona and neutral H and the auroral oval | FOV - image auroral oval from apogee (8o). Spatial Res. - 50 km. Spectral Resolution - Separate cold geocorona H from hot proton precipitation ([[Delta]][[lambda]]~2 nm near 121.6 nm); separate 130.4 nm and 135.6 nm electron aurora emissions. Image Time - resolve auroral activity (2 - 5 min) |
RPI | Radio sounder to measure electron densities and locate magnetospheric boundaries |
Image Time - resolve changes in boundary locations (1 min ). Spatial resolution - resolve density structures at the magnetopause and plasmapause (500 km). Density range - determine electron density from magnetopause to inner plasmasphere (0.1-105 cm-3) |
1.3.2 Science Closure and Analysis. The IMAGE data will be used to answer the key science questions posed in Section 1.2. In the following, we give examples of the analysis of time sequences and the correlation of the images from different instruments that will be performed.
a. Are the structures in the cusp indicative of pulsed reconnection? This question will be answered by combining images from two instruments as a function of time. When the satellite is at high altitude in a position for the RPI to view the cusp, it will provide pictures of the shape of the cusp with high time resolution. The FUV will show us the footprint in the ionosphere. Figure 1.3.2 shows a simulated proton aurora image from the FUV spectrometer for moderate magnetospheric activity (Kp=4). The wavelength range is 121.6-122.8 nm. Local noon is down, and the cusp is clearly visible as an isolated emission patch centered on noon. When the satellite is at low altitude and flying near the cusp, NAI will provide a different picture of the cusp, but one that can also be correlated with the FUV images to determine its dynamics, whether steady or pulsating.
Figure 1.3.2 A simulated proton aurora image from the FUV spectrometer for moderate magnetospheric activity (Kp=4).
b. What are the processes that determine the structure and dynamics of the plasmasphere and plasmapause? The EUV images will show the structure of the plasmasphere directly (Figure 1.3.3). A 3-D, time-dependent image of the plasmasphere will be obtained by applying the deconvolution techniques described in the next section for NAI to these EUV images and combining the result with deconvolved RPI images. The deconvolved NAI images will give the position of the ring current relative to the plasmapause.
In the RPI data the quantity measured is the time delay, which is related to the path integral of the index of refraction. Because the index of refraction is a nonlinear function of the density, the deconvolution must be done iteratively. For most of the magnetospheric echoes to be obtained by IMAGE, the sounding frequency will be well above the plasma frequency over most of the propagation path. The iteration therefore converges very rapidly, yielding accurate density profiles.
The simultaneous FUV images will link the plasmapause shape with auroral activity. By combining the information from all these images, we will not only determine for the first time the global structure of the plasmapause but also its connectivity to other regions.
Fig. 1.3.3 Simulated EUV image of plasmasphere from the IMAGE spacecraft at an altitude of 7 Earth radii over the north pole.Based on model of Rasmussen et al., 1993.
c. How and where is plasma injected into the inner magnetosphere or ring current? NAI images are line-of-sight integral measurements, which can be deconvolved to produce ion pitch-angle distributions at the equator. The first step in this process is to expand the sought-after function in terms of coefficients of separable expansion functions. The second step is to use a regularization procedure based upon Bayesian statistics and the principle of minimum cross entropy to determine the coefficients of the expansion by satisfying a variational equation. This procedure has been well-developed within our team and has been applied to many different sets of simulated NAI images.
An example of the results is shown in Fig. 1.3.4, in which the simulated ion fluxes were produced using the 3-D storm model of Fok et al. [1995] with noise proportional to the square root of the counts included The pixels in the NAI images are 8 x 8 degrees with a sensitivity representative of the proposed NAI instrument. The perspective is from the noon-midnight meridian plane near apogee at 7 RE at midnight at a latitude of 45 degrees. The fourth row shows the deconvolved equatorial ion distributions integrated over pitch angle. The white areas are the peak fluxes, which exceed the values shown on the color bar. The deconvolved results clearly show (1) an enhancement of the ion flux in the injection with time, (2) the inward motion of the peak flux with time, and (3) the spread of the flux toward the dayside with time. In the bottom row, equatorial distributions for three different pitch angles at time 3 are shown.
Figure 1.3.4 Model ion source, neutral atom fluxes, simulated NAI images, and deconvolved ion source for 1.7 keV H during a magnetic storm on May 2, 1986 from a satellite at 00 MLT, radial distances 6.4 RE, 61 degrees latitude (Time 1, 08 UT), 7.0 RE, 45 degrees (Time 2, 10 UT) and 6.4 RE, 29 degrees (Time 3, 12 UT). First Row. Model equatorial ion sources out to 6.5 RE. Second row. ENA fluxes in a 90 by 90 degrees FOV. Third row. Counts as recorded in the IMAGE NAI instrument. Fourth row. Deconvolved equatorial ion flux integrated over pitch angle, to be compared with the model input shown in the first row. Fifth row. Deconvolved ion distributions for three pitch angles at Time 3.